Numerical Predictions of Scarfing on Performance of S-Shaped Nozzle with Asymmetric Lobe
Author:
Affiliation:
1. School of Energy and Power Engineering, Beihang University, 100191 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35222
Reference28 articles.
1. Supersonic-ejector characteristics using a Petal nozzle
2. Experimental and numerical research on high pumping performance mechanism of lobed exhauster-ejector mixer
3. Experimental study on mixing enhancement by petal nozzle in supersonic flow
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